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Untitled - Aerobib - Universidad Politécnica de Madrid

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13.6. CONTINUITY EQUATIONS 309<br />

Chemical reactions take place only on the flame surface r = r l , which acts as<br />

a sink for fuel and oxidizer and as a source for the combustion products. Therefore<br />

one obtains for each different chemical species an equation similar to Eq. (13.10). In<br />

this equation ρ must be substituted by the partial <strong>de</strong>nsity ρ i = ρY i corresponding to<br />

species A i , v by velocity v i = v + v di , where v di is the radial diffusion velocity of the<br />

species, and m must be substituted by the partial flow m i of the species. Thus<br />

4πr 2 ρY i v i = m i , (i = 1, 2, 3). (13.11)<br />

Moreover, the following evi<strong>de</strong>nt conditions must be satisfied<br />

∑<br />

Y i v i = v, (13.12)<br />

i<br />

∑<br />

m i = m. (13.13)<br />

i<br />

Equation (13.11) is valid for each species A i , as long as r does not cross the flame.<br />

Let us now apply these equations separately to the interior and exterior regions<br />

of the flame.<br />

Interior region r s ≤ r ≤ r l<br />

In this region only fuel vapours and inert gases exist, since the incoming oxygen is<br />

entirely consumed as it reaches the flame without crossing it.<br />

Equation (13.11) applied to the fuel vapours A 1 gives<br />

4πr 2 ρY 1 v 1 = m 1 = m, (13.14)<br />

since on the droplet surface the mass flow m is the mass flow m 1 of the fuel produced<br />

by evaporation.<br />

By comparing (13.9) and (13.14)<br />

Y 1 v 1 = v. (13.15)<br />

Equation (13.12) gives<br />

Y 1 v 1 + Y 2 v 2 = v. (13.16)<br />

From Eqs. (13.15) and (13.16) results<br />

v 2 = 0, (13.17)<br />

that is to say within the interior region the inert gases are at rest and the fuel vapours<br />

diffuse through them towards the flame.

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